METHOD FOR DIAGNOSING SURGING OF GAS TURBINE ENGINE COMPRESSOR AND DEVICE FOR ITS IMPLEMENTATION Russian patent published in 2017 - IPC F04D27/02 

Abstract RU 2638896 C1

FIELD: engines and pumps.

SUBSTANCE: method additionally comprises measuring the vibration of the rotor behind the low-pressure compressor and behind the high-pressure compressor, mean square deviation of vibrations is calculated and compared with its threshold value, wavelet vibration transformation is calculated, and the extrema frequencies are compared with reference values, the threshold values of the working parameters are corrected if wavelet transformation of vibration extrema frequencies match with reference values. The device contains a rotor vibration sensor behind the low-pressure compressor and a rotor vibration sensor behind high-pressure compressor connected to microcontroller, which connected with the output to the antisurge system.

EFFECT: increased reliability and speed for determining the beginning of surging at all engine operation modes.

2 cl, 1 dwg

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RU 2 638 896 C1

Authors

Tokarev Vladimir Petrovich

Kudashov Dmitrij Dmitrievich

Dates

2017-12-18Published

2017-03-14Filed